| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:1181986078:1986 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:1181986078:1986?format=raw |
LEADER: 01986nam a22004817a 4500
001 42814679
003 OCoLC
005 19991112105104.0
008 991112s1998 vau b f000 0 eng d
035 $a(GPO)99029418
037 $a19980232887$bNASA
040 $aGPO$cGPO$dDLC$dMvI
049 $aORE1
074 $a0830-H-15 (MF)
086 0 $aNAS 1.60:208464
086 0 $aNAS 1.60:208464
100 1 $aLallman, Frederick J.
245 12 $aA method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane$h[microform] /$cFrederick J. Lallman, John B. Davidson, and Patrick C. Murphy.
246 2 $aMethod for integrating thrust vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane.
260 $aHampton, Va. :$bNational Aeronautics and Space Administration, Langley Research Center ;$aSpringfield, VA :$bNational Technical Information Service, distributor,$c[1998]
300 $a1 v.
490 1 $a[NASA technical paper] ;$vNASA/TP-1998-208464.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1998]$e1 microfiche.
500 $aShipping list no.: 1999-0479-M.
650 7 $aThrust vector control.$2nasat.
650 7 $aFighter aircraft.$2nasat.
650 7 $aFlight control.$2nasat.
650 7 $aFeedback control.$2nasat.
650 7 $aDirectional control.$2nasat.
650 7 $aControl stability.$2nasat.
650 7 $aAngular acceleration.$2nasat.
650 7 $aAngle of attack.$2nasat.
650 7 $aF-18 aircraft.$2nasat.
700 1 $aDavidson, John B.
700 1 $aMurphy, Patrick C.
710 2 $aLangley Research Center.
830 0 $aNASA technical paper ;$v208464.
907 $a.b2039228x$bvdo $cv
902 $a010129
998 $b2$c991231$dm$ea$fv$g2
935 $atmp97148599
937 $aAssessment exclusion record.
945 $lvdonf$e1